Mh-53e Helicopter Parts

(Page 180) End item NSN parts page 180 of 238
Part Number
NSN
NIIN
117367A Nonmetallic Hose
006767936
117370 Fluid Filter Element
002871912
117370A Fluid Filter Element
002871912
11737527-1 Setscrew
008208367
117377 Extractor Post Fuseholder
010059621
117381 Extractor Post Fuseholder
010929400
11738989 Induct Wire Wound Fixed Resistor
000805899
11741583 Diode Semiconductor Device
000487106
117436-019 Solid Rivet
001176813
1174423 Fluid Filter Element
002380033
11746931 Transistor
010169906
11751-1 Electrical Plug Connector
002578321
117526PC478 Pipe Bushing
002783167
117530PC748 Pipe Bushing
002783167
117676-000 Telephone Jack
001924789
117684-000 Radio Frequency Cable
008125034
117754-02 Electrical Connector Retainer
009324560
11776963 Cable Assembly
010737428
11778543 Transistor
010169906
11779 Nonmetallic Hose
004509156
Page: 180 ...

Helicopter, Mh-53e

Picture of Mh-53e Helicopter

The Sikorsky CH-53E Super Stallion is the largest and heaviest helicopter in the United States military. As the Sikorsky S-80 it was developed from the CH-53 Sea Stallion, mainly by adding a third engine, adding a seventh blade to the main rotor and canting the tail rotor 20 degrees. It was built by Sikorsky Aircraft for the United States Marine Corps. The less common MH-53E Sea Dragon fills the United States Navy's need for long range minesweeping or Airborne Mine Countermeasures (AMCM) missions, and perform heavy-lift duties for the Navy. Under development is the CH-53K King Stallion, which will be equipped with new engines, new composite material rotor blades, and a wider aircraft cabin.

The CH-53 was the product of the U.S. Marines' "Heavy Helicopter Experimental" (HH(X)) competition begun in 1962. Sikorsky's S-65 was selected over Boeing Vertol's modified CH-47 Chinook version. The prototype YCH-53A first flew on 14 October 1964. The first CH-53As were powered by two General Electric T64-GE-6 turboshaft engines with 2,850 shp (2,125 kW) and had a maximum gross weight of 46,000 lb (20,865 kg) including 20,000 lb (9,072 kg) in payload.

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